Partially unshrouded swirler for combustion chambers

Claim 2

A burner construction including: an end cap having a primary fuel nozzle therein; side walls extending downstream from the cap to define the combustion chamber; a tube extending axially downstream from said cap and centrally of the combustion chamber for secondary fuel and air; a secondary nozzle in said cap for discharging fuel into said tube; a swirler at the downstream end of said tube, said swirler having a plurality of radially extending swirl vanes with leading edges and trailing edges and shaped to impart a swirl to the fuel and air mixture passing over said vanes; and a shroud extending over only a portion of the vanes from the leading edge and leaving the trailing edges and the outer ends of the vanes adjacent thereto unshrouded, thereby to provide a wider distribution of the fuel and air passing over said vanes, the unshrouded portions of the vanes increasing in length radially at their outer ends to impart a greater swirl to the secondary fuel and air mixture passing over the vanes.

Claim 3

A burner construction as in claim 1 in which the swirler has a central sleeve with the vanes extending generally radially outward therefrom.

Claim 4

A burner construction as in claim 1 in which the shroud extends for less than half the length of the vane.

Claim 5

A burner construction including: an end cap having the primary fuel nozzle therein; side walls extending downstream from the cap to define a combustion chamber; axially extending tubes on the inner surface of the side walls for guiding air forwardly of the side walls for heating this air; said tube discharging into the upstream end of the combustion chamber adjacent to the end cap; a tube extending axially downstream from said cap and centrally of the combustion chamber for delivery of secondary fuel and air, said tube extending substantially to the end of the primary combustion zone; a secondary nozzle in said cap for discharging fuel into said tube to mix with the air therein and a swirler at the downstream end of said tube, said swirler including a plurality of swirl vanes having leading edges and trailing edges and shaped to impart a swirl to the fuel and air mixture passing said vanes, said vanes extending generally radially of the tube; and a shroud extending over a portion only of the vanes from the leading edge but leaving the trailing edges and the outer ends of the vanes adjacent thereto unshrouded for imparting a wider conical spray angle to the fuel and air discharging from said tube.

Claim 6

A burner construction including: an end cap having the primary fuel nozzle therein; side walls extending downstream from the cap to define a combustion chamber; axially extending tubes on the inner surface of the side walls for guiding air forwardly of the side walls for heating this air; said tube discharging into the upstream end of the combustion chamber adjacent to the end cap; a tube extending axially downstream from said cap and centrally of the combustion chamber for delivery of secondary fuel and air, said tube extending substantially to the end of the primary combustion zone; a secondary nozzle in said cap for discharging fuel into said tube to mix with the air therein and a swirler at the downstream end of said tube, said swirler including a plurality of swirl vanes having leading edges and trailing edges and shaped to impart a swirl to the fuel and air mixture passing said vanes, said vanes extending generally radially of the tube; and a shroud extending over a portion only of the vanes from the leading edge but leaving the trailing edges and the outer ends of the vanes adjacent thereto unshrouded for imparting a wider conical spray angle to the fuel and air discharging from said tube.

Claim 7

A burner construction as in claim 4 in which the unshrouded portions of the vanes increase in length toward the trailing edge to cause a wider conical distribution of the fuel and air mixture.